Tethered unmanned aerial vehicle system

ABSTRACT

In one aspect, an example system includes: (i) a base including a bottom surface and a first coupling-point; (ii) a vertically-oriented elongate structure comprising a lower end, an upper end, and an inner channel, wherein the inner channel comprises an upper access-point disposed proximate the upper end, wherein the base is coupled to the elongate structure proximate the lower end; (iii) a deployable cushioning-device coupled to the elongate structure; and (iv) a tether comprising a first portion, a second portion, a third portion, and a fourth portion, wherein the first portion is coupled to the first coupling-point, the second portion is coupled to a second coupling-point of the UAV, the third portion extends through the inner channel, the fourth portion extends from the upper access-point to the second coupling-point, and the fourth portion has a length that is less than a distance between the upper access-point and the bottom surface.

RELATED DISCLOSURE

This disclosure claims priority to U.S. Provisional Pat. App. No.62/273,728 filed on Dec. 31, 2015, the content of which is herebyincorporated by reference in its entirety.

USAGE AND TERMINOLOGY

In this disclosure, unless otherwise specified and/or unless theparticular context clearly dictates otherwise, the terms “a” or “an”mean at least one, and the term “the” means the at least one.

BACKGROUND

Unless otherwise specified, the materials described in this section arenot prior art to the claims in this disclosure and are not admitted tobe prior art by inclusion in this section.

Advancements in technology and computing have contributed to a recentincrease in the development and overall use of unmanned aerial vehicles(UAVs). A UAV is an aircraft that can operate without an on-board humanoperator. Sometimes referred to as a “drone” or an “unmanned aerialsystem,” a UAV can take various forms, such as a helicopter, quadcopter,fixed-wing aircraft, blimp, or glider, and can be used for variousapplications, such as capturing an image or video of an area from anaerial perspective.

A UAV can operate in one or more modes, such as a remote-control mode,an autonomous mode, or a semi-autonomous mode. While the UAV isoperating in a remote-control mode, a remotely-located operator canoperate the UAV. While the UAV is operating in an autonomous mode, acomputing system onboard the UAV can operate the UAV. Finally, while theUAV is operating in a semi-autonomous mode, a remotely-located operatorcan cause the UAV to perform some operations, and a computing systemonboard the UAV can cause the UAV to perform other operations. Forinstance, the operator can instruct the UAV to navigate to a particularlocation, and the computing system can cause the UAV to autonomouslynavigate to that location.

SUMMARY

In one aspect, an example system is disclosed. The system includes: abase comprising a bottom surface and a first coupling-point; avertically-oriented elongate structure comprising a lower end, an upperend, and an inner channel, wherein the inner channel comprises an upperaccess-point disposed proximate the upper end, wherein the base iscoupled to the elongate structure proximate the lower end; a UAVcomprising a second coupling-point; and a tether comprising a firstportion, a second portion, a third portion, and a fourth portion,wherein (i) the first portion is coupled to the first coupling-point,(ii) the second portion is coupled to the second coupling-point, (iii)the third portion extends through the inner channel, (iv) the fourthportion extends from the upper access-point to the secondcoupling-point, and (v) the fourth portion has a length that is lessthan a distance between the upper access-point and the bottom surface.

In another aspect, an example system for use with a UAV is disclosed.The system includes: a base comprising a first coupling-point; avertically-oriented elongate structure comprising a lower end, an upperend, and an inner channel, wherein the inner channel comprises an upperaccess-point disposed proximate the upper end, wherein the base iscoupled to the elongate structure proximate the lower end; a landingstructure constructed and arranged for receiving the UAV, wherein thelanding structure is coupled to the elongate structure proximate theupper end; and a tether comprising a first portion, a second portion, athird portion, and a fourth portion, wherein (i) the first portion iscoupled to the first coupling-point, (ii) the second portion is coupledto a second coupling-point of the UAV, (iii) the third portion extendsthrough the inner channel, and (iv) the fourth portion extends from theupper access-point to the second coupling-point.

In a further aspect, another example system for use with a UAV isdisclosed. The system includes: a base comprising a bottom surface and afirst coupling-point; a vertically-oriented elongate structurecomprising a lower end, an upper end, and an inner channel, wherein theinner channel comprises an upper access-point disposed proximate theupper end, wherein the base is coupled to the elongate structureproximate the lower end; a landing structure constructed and arrangedfor receiving the UAV, wherein the landing structure is coupled to theelongate structure proximate the upper end; and a tether comprising afirst portion, a second portion, a third portion, and a fourth portion,wherein (i) the first portion is coupled to the first coupling-point,(ii) the second portion is coupled to a second coupling-point of theUAV, (iii) the third portion extends through the inner channel to theupper access-point, (iv) the fourth portion extends from the upperaccess-point, through the opening, and to the second coupling-point, and(v) the fourth portion has a length that is less than a distance betweenthe upper access-point and the bottom surface.

In yet another aspect, an example system for use with a UAV isdisclosed. The UAV includes: a base comprising a bottom surface and afirst coupling-point; a vertically-oriented elongate structurecomprising a lower end, an upper end, and an inner channel, wherein theinner channel comprises an upper access-point disposed proximate theupper end, wherein the base is coupled to the elongate structureproximate the lower end; a deployable cushioning-device coupled to theelongate structure; a tether comprising a portion that extends from theupper access-point to the UAV, the portion having a length that is lessthan a distance between the upper access-point and the bottom surface;and a computing system configured for performing a set of actscomprising: detecting abnormal operation of the UAV; and responsive todetecting abnormal operation of the UAV, causing the deployablecushioning-device to deploy.

In another aspect, an example non-transitory computer-readable mediumfor use with a system is disclosed. The system includes: a basecomprising a bottom surface and a first coupling-point; avertically-oriented elongate structure comprising a lower end, an upperend, and an inner channel, wherein the inner channel comprises an upperaccess-point disposed proximate the upper end, wherein the base iscoupled to the elongate structure proximate the lower end; a deployablecushioning-device coupled to the elongate structure; and a tethercomprising a portion that extends from the upper access-point to theUAV, the portion having a length that is less than a distance betweenthe upper access-point and the bottom surface. The examplenon-transitory computer-readable medium has stored thereon programinstructions that when executed cause performance of a set of actscomprising: detecting abnormal operation of the UAV; and responsive todetecting abnormal operation of the UAV, causing the deployablecushioning-device to deploy.

In another aspect, an example method for use with a system is disclosed.The system includes: a base comprising a bottom surface and a firstcoupling-point; a vertically-oriented elongate structure comprising alower end, an upper end, and an inner channel, wherein the inner channelcomprises an upper access-point disposed proximate the upper end,wherein the base is coupled to the elongate structure proximate thelower end; a deployable cushioning-device coupled to the elongatestructure; and a tether comprising a portion that extends from the upperaccess-point to the UAV, the portion having a length that is less than adistance between the upper access-point and the bottom surface. Theexample method includes: detecting abnormal operation of the UAV; andresponsive to detecting abnormal operation of the UAV, causing thedeployable cushioning-device to deploy.

In a further aspect, an example system for use with a UAV is disclosed.The example system includes: a base comprising a bottom surface and afirst coupling-point; a vertically-oriented elongate structurecomprising a lower end, an upper end, and an inner channel, wherein theinner channel comprises an upper access-point disposed proximate theupper end, wherein the base is coupled to the elongate structureproximate the lower end; a cushion-component coupled to the elongatestructure; and a tether comprising a portion that extends from the upperaccess-point to the UAV, the portion having a length that is less than adistance between the upper access-point and the bottom surface.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a simplified block-diagram of an example computing device.

FIG. 2 is an illustration of an example UAV system.

FIG. 3 is another illustration of the example UAV system.

FIG. 4 is a flow chart of an example method.

DETAILED DESCRIPTION I. Overview

As discussed above, a UAV can fly without an onboard human operator. Insome instances though, a UAV can malfunction and lose the ability to flyproperly. As a result, the UAV can fall to the ground and crash, whichcan potentially injure a person or damage property. Disclosed herein isa tethered UAV system that can help avoid such injuries and/or damages.

In one example, a tethered UAV system can have a base with avertically-oriented elongate structure that positions a portion of atether connected to a UAV at a height that can limit a position of thetethered UAV. Within the system, the tether can extend from the base upthrough an inner channel of the vertically-oriented elongate structureand connect to a UAV from the top of the elongate structure. As aresult, the tether can limit the distance that the UAV can fly away fromthe top of the elongate structure. Thus, the tether may constrain theUAV to a volume centered at the top of the elongate structure andextending radially outward by an extent defined by the tether. In someinstances, the tether can have a portion of the tether extending fromthe top of the elongate structure to the UAV can have a length that isless than the height of the elongate structure, which can enable thetether to reduce the chance of the UAV reaching people or objects on theground nearby. With this arrangement, even if the UAV malfunctions andloses the ability to fly property, rather than crashing into the ground,the combination of the elongate structure and tether can cause the UAVto swing like a pendulum from atop the elongate structure, andpotentially miss hitting people or objects.

As discussed above, a tethered UAV system can limit a UAV from reachingthe ground. Given this, the UAV may be unable to land on the ground.However, disclosed herein is a tethered UAV system that can help enablea tethered UAV to land somewhere else. In one example, a tethered UAVsystem can include a landing structure that is configured and arrangedto receive the tethered UAV. The landing structure can provide aplatform for the UAV to land and can have various configurations, suchas a bowl-shaped portion constructed to catch a tethered UAV duringlanding. In some examples, the landing structure is connected near theupper end of the elongate structure and can also serve as a take-offplatform for the tethered UAV to initiate flight.

Additionally, UAVs can be costly and often carry expensive equipment(e.g., cameras, sensors). Although a tethered UAV system can help reducea tethered UAV from colliding with property located on the ground, thetether can still cause the UAV to swing into the vertically-orientedelongate structure as a result of a malfunction of the UAV, which candamage the UAV or equipment located on the UAV. Disclosed herein is atethered UAV system that can help avoid such damage.

In an example, a tethered UAV system can include a deployablecushioning-device positioned on the outer surface of thevertically-oriented elongate structure. The deployable cushioning-devicecan help absorb the impact of a collision between the tethered UAV andthe elongate structure and potentially reduce damage to the UAV. In someinstances, a cushioning-device can have a deployable configuration thatenables a computing system operating in the tethered UAV system todetect abnormal operation of the UAV and to cause the deployablecushioning-device to deploy in response. In this way, a deployablecushioning-device can stay stored in a position on the elongatestructure and deploy in a manner similar to an air-bag (e.g., byinflating) to potentially reduce damage to the UAV and/or the elongatestructure during a collision.

II. Example Architecture

A. Computing Device

FIG. 1 is a simplified block-diagram of an example computing device 100that can perform various acts and/or functions, such as those describedin this disclosure. Computing device 100 can include various components,such as processor 102, data storage unit 104, communication interface106, and/or user interface 108. The components can be connected to eachother (or to another device, system, or other entity) via connectionmechanism 110.

In this disclosure, the term “connection mechanism” means a mechanismthat facilitates communication between two or more devices, systems, orother entities. A connection mechanism can be a relatively simplemechanism, such as a cable or system bus, or a relatively complexmechanism, such as a packet-based communication network (e.g., theInternet). In some instances, a connection mechanism can include anon-tangible medium (e.g., where the connection is wireless).

Processor 102 can include a general-purpose processor (e.g., amicroprocessor) and/or a special-purpose processor (e.g., a digitalsignal processor (DSP)).

Data storage unit 104 can include one or more volatile, non-volatile,removable, and/or non-removable storage components, such as magnetic,optical, or flash storage, and/or can be integrated in whole or in partwith processor 102. Further, data storage unit 104 can take the form ofa non-transitory computer-readable storage medium, having stored thereonprogram instructions (e.g., compiled or non-compiled program logicand/or machine code) that, when executed by processor 102, causecomputing device 100 to perform one or more acts and/or functions, suchas those described in this disclosure. As such, computing device 100 canbe configured to perform one or more acts and/or functions, such asthose described in this disclosure. Such program instructions can defineand/or be part of a discrete software application. In some instances,computing device 100 can execute program instructions in response toreceiving an input, such as from communication interface 106 and/or userinterface 108. Data storage unit 104 can also store other types of data,such as those types described in this disclosure.

Communication interface 106 can allow computing device 100 to connect toand/or communicate with another other entity according to one or moreprotocols. In one example, communication interface 106 can be a wiredinterface, such as an Ethernet interface or a high-definitionserial-digital-interface (HD-SDI). In another example, communicationinterface 106 can be a wireless interface, such as a cellular or WI-FIinterface. In this disclosure, a connection can be a direct connectionor an indirect connection, the latter being a connection that passesthrough and/or traverses one or more entities, such as such as a router,switcher, or other network device. Likewise, in this disclosure, atransmission can be a direct transmission or an indirect transmission.

User interface 108 can facilitate interaction between computing device100 and a user of computing device 100, if applicable. As such, userinterface 108 can include input components such as a keyboard, a keypad,a mouse, a touch-sensitive panel, a microphone, and/or a camera, and/oroutput components such as a display device (which, for example, can becombined with a touch-sensitive panel), a sound speaker, and/or a hapticfeedback system. More generally, user interface 108 can include hardwareand/or software components that facilitate interaction between computingdevice 100 and the user of the computing device 100.

Computing device 100 can take various forms, such as a workstationterminal, a desktop computer, a laptop, a tablet, and/or a mobile phone.

B. Tethered UAV System

FIG. 2 is an illustration of an example UAV system 200. System 200includes base 202, elongate structure 204, UAV 206, tether 208, andlanding structure 210, but can also include more or less componentswithin examples. For instance, system 200 can include components notshown in FIG. 2, such as a computing system in or on base 202. In thisdisclosure, the term “computing system” means a system that includes atleast one computing device. As such, system 200 can be configured toperform various acts and/or functions, including those described in thisdisclosure (including in the accompanying drawings) in accordance with aset of instructions specified by such a computing system.

Base 202 is shown as a vehicle in FIG. 2, but can exist in othernon-stationary or stationary configurations in some examples. As shown,base 202 includes bottom surface 212, and spooling mechanism 214configured with first coupling-point 216. Bottom surface 212 correspondsto the bottom of a wheel of base 202 and represents a lower portion ofbase 202 located adjacent or nearby the ground. In other examples,bottom surface 212 can correspond to other portions of base 202,including portions located farther from the ground.

Spooling mechanism 214 is a mechanical structure coupled to base 202that can store and adjust a length of tether 208 through automatic ormanual means. For example, spooling mechanism 208 may include a reelthat rotates to either wind the tether 208 around the reel, and therebydecrease the length of the portion of the tether 208 that is not woundaround the reel, or unwind the tether 208, and thereby increase thelength of the portion of the tether 208 that is not wound around thereel. Tether 208 is connected to spooling mechanism 214 at firstcoupling-point 216. As such, spooling mechanism 214 can be configured toautomatically adjust the length of tether 208 via mechanical operationbased on user input or can also enable a human operator to manuallyadjust tether 208 (e.g., by winding/unwinding the spooling mechanism viarotation of a handle or by causing an electric motor to operate so as toengage the spooling mechanism and effect such winding/unwinding). Insome instances, spooling mechanism 214 can also serve as storage fortether 208 during navigation by base 202. Moreover, in some examples,the tether 208 may connect to base 202 at other positions (e.g.,directly to base 202).

In some examples, base 202 can have other components, such as a powersource and communication components. For instance, UAV 206 cancommunicate and receive power from components positioned on base 202through tether 208.

As shown in FIG. 2, elongate structure 204 can be a vertically-orientedadjustable mast coupled to base 202. The elongate structure is shown inFIG. 2 in a cutaway form that illustrates the interior of elongatestructure 204. As an adjustable mast, elongate structure 204 can changeorientation and position, extend upward, adjust angle of orientation,and collapse into a storable position using pneumatics, for example. Inother examples, elongate structure 204 can have other configurations,such as multiple structures (e.g., poles) connected to base 202.Elongate structure 204 connects to base 202 at lower end 218 and extendsin a vertical orientation from base 202 with upper end 220 of elongatestructure 204 positioned opposite of lower end 218. Additionally,elongate structure 204 can include inner channel 222 with loweraccess-point 224 to inner channel 222 disposed proximate lower end 218,and upper access-point 226 of inner channel 222 disposed proximate upperend 220. Upper-access point 226 is shown having a circular opening toenable full rotation of tether 208 as UAV 206 navigates an environmentin various directions, but can have other configurations in someexamples.

As shown in FIG. 2, tether 208 may be routed through the inner channel222 of elongate structure 204. Thus, tether 208 may enter the loweraccess-point 224, pass through inner channel 222 and exit through upperaccess-point 226. As such, the spooling mechanism 214 may be situatedexterior to the elongate structure 204 (e.g., mounted to base 202proximate the lower end 218 of the elongate structure 204, as shown inFIG. 2). However, in some examples, the spooling mechanism may bemounted at other locations. For example, the spooling mechanism may besituated within the base 202 or within the elongate structure 204itself. As such, the lower access-point 224 may not provide access tothe inner channel 222 from an exterior of the base 202. For instance, ifthe spooling mechanism 214 is mounted within the base 202, below thelower end 218 of the elongate structure 204, an access point to theinner channel 222 may be provided that is interior to the base 202 tothereby provide a path for the tether to pass between the such aninterior-mounted spooling mechanism and the inner channel 222 of theelongate structure 204. Moreover, in some cases, the spooling mechanismmay be disposed within the elongate structure 204 itself, in which casethe inner channel 222 may only extend between the upper access-point 226and the location of such a spooling mechanism. Further, in an example inwhich the spooling mechanism is situated proximate the upper end 220 ofthe elongate structure 204, the tether 208 may not pass through theinner channel 222 at all. In any of these configurations, operation ofthe spooling mechanism 214 to wind/unwind the tether 208 can be used tocontrol the length of the tether 208 that extends from proximate the topend 220 of the elongate structure 204 (e.g., at the upper access-point226) to the UAV 206, and thereby limit the maximum separation distancebetween the top end 220 of the elongate structure 204 and the UAV 206.

Elongate structure 204 further includes deployable cushioning-device 228connected to an outer surface of elongate structure 204. Deployablecushioning-device 228 can potentially reduce damage to UAV 206 and/orelongate structure 204 in the event UAV 206 collides with elongatestructure 204. For example, if UAV 206 ceases normal flying operations(e.g., due to a malfunction) the tether 208 may cause the UAV 206 toswing into the elongate structure 204. For instance, a computing systemof system 200 can detect abnormal operation of tethered UAV 206 andcause deployable cushioning-device 228 to inflate using a gaseoussubstance in response. The deployable cushioning-device 228 may inflateby changing from having a first volume of gaseous substance inside tohaving a second volume of gaseous substance with the second volume beinggreater than the first volume. The deployable cushioning-device 228 caninclude a set of deployable cushioning components that together extendaround the outer surface of elongate structure 204 at various positions,for example. In some examples, elongate structure 204 can includecushioning components that do not require inflating or other type ofpreparation by system 200 before use. For instance, stationarycushioning components may be mounted on the exterior surface of elongatestructure 204.

To help allow deployable cushioning-device 204 to provide suchfunctionality, deployable cushioning-device 204 can be positioned on theelongate structure 204 at a height such that a length of the fourthportion 240 is greater than or equal to a first distance between theupper access-point 226 and an upper end 246 of the deployablecushioning-device 228, and is also less than or equal to a seconddistance between the upper access-point 226 and a lower end 248 of thedeployable cushioning-device 228.

System 200 further includes UAV 206 tethered to base 202 via tether 208.UAV 206 can be any type of aircraft capable of operation without anon-board human operator. For instance, in some examples, a humanoperator can control navigation of UAV 206 via a physically separateremote control that can provide control instructions to UAV 206 via awired or wireless connection. As shown in FIG. 2, UAV 206 can beconfigured with second coupling-point 228 that serves as the connectionpoint for connecting tether 208 to UAV 206. Within examples, secondcoupling-point 228 can have various locations on UAV 206, which candepend on the configuration of UAV 206. As such, UAV 206 can havevarious configurations, such as a helicopter, quadcopter, fixed-wingaircraft, blimp, or glider, and can operate in various modes, such as aremote-control mode, an autonomous mode, or a semi-autonomous mode.

UAV 206 can include camera 230 configured to capture video and/or imagesfrom an aerial perspective. UAV 206 can include other components, suchas a power source (e.g., battery) and a computing system locatedon-board. In some examples, UAV 206 can also be configured to receivepower from a power source located on base 202 through apower-distribution connection positioned within tether 208. This canenable UAV 206 to have a reduced weight since an on-board battery is notrequired. During operation, UAV 206 can transmit and receivecommunications, such as sensor data, images, video, and controlinstructions, using tether 208 or through a wireless connection withanother computing system, such as the computing system of base 202.

System 200 includes tether 208 that serves as a connecting link betweenbase 202 and UAV 206. Tether 208 can include various materials,including materials that enable elastic extension as well as materialsthat enable transfer of electrical power or communications between thecomputing systems of base 202 and UAV 206. In some examples, tether 208can include multiple components constructed together.

Referring to FIG. 3, tether 208 is divided into first portion 234,second portion 236, third portion 238, and fourth portion 240. Firstportion 234 of tether 208 extends from first coupling-point 216 intolower access point 224, and second portion 236 is the portion of tether208 that connects to UAV 206 at second coupling point 228. Although,tether 208 can connect to base 202 and UAV 206 at different positions.For instance, first portion 234 of tether 208 can connect directly tobase 202 without spooling mechanism 214. Third portion 238 of tether 208starts from lower access-point 224 and extends through inner channel 222of elongate structure 204 to the upper access-point 226 of elongatestructure 204. The fourth portion 240 of tether 208 extends from upperaccess-point 226 of elongate structure 204 to second portion 236 oftether 208 positioned at second coupling-point 228 on UAV 206.

In some examples, fourth portion 240 of tether 208 can have a lengththat is less than a distance between upper access-point 226 of elongatestructure 204 and bottom surface 212 of base 202. At this length orshorter, tether 208 can suspend UAV 206 above the ground as a result ofa malfunction of UAV 206 during flight. As noted elsewhere, the lengthof the fourth portion 240 may be controlled via operation of thespooling mechanism 214 to wind/unwind the tether 208.

System 200 can further include landing structure 210 that is constructedand arranged for receiving UAV 206. Landing structure 210 can provide astructure for UAV 206 to land and also serve as a take-off platform forUAV 206 to initiate flight, for example. As shown in FIG. 2, landingstructure 210 can be connected proximate upper end 220 of elongatestructure 204. As shown in FIG. 3, landing structure 210 can includeopening 242 that enables tether 208 (or any portion thereof) to extendthrough landing structure 210. In some examples, opening 242 can have acircular configuration to enable full rotation of tether 208 during UAV206 operation and can also be positioned proximate to upper access-point226 of elongate structure 204.

Landing structure 210 is shown having a bowl-shaped portion 244constructed and arranged for receiving UAV 206, but can have otherconfigurations in some examples. Bowl-shaped portion 244 can includemesh or nylon netting, for example, to assist in catching a landing UAV206. In one example, landing structure 210 can have a net disposedaround a perimeter of landing structure 210. In other examples, landingstructure 210 can include other structures and materials, such ascombinations of hard and soft materials. For instance, landing structure210 can have collapsible portions that can collapse and extend outwardas controlled by the computing system of system 200.

As shown, landing structure 210 can be mounted to elongate structure 204so as to entirely surround the outer sidewall surface of the elongatestructure 204 near the top end 220. However, in some examples, thelanding structure 210 may be positioned adjacent a portion of the outersidewall surface without entirely surrounding the elongate structure204.

Landing structure 210 can also include a coupling portion that extendsaround the upper end 220 of the elongate structure 204 to facilitatecoupling the landing structure 210 to the elongate structure 204. Thecoupling portion can take various forms. For example, the couplingportion can be a lip that engages a corresponding recess on the elongatestructure 204. However, other coupling techniques can be used as well.

III. Example Operations

The system 200 and/or components thereof can perform various acts. Theseacts and related features will now be described. A computing system ofsystem 200 can monitor and detect when UAV 206 is operating abnormallyduring operation. In response to detecting this, the computing systemcan initiate actions, such as causing the deployable cushioning-device228 to inflate or preparing landing structure 210 for use. For example,computing system can interpret abnormal operation of UAV 206 as apotential malfunction by UAV 206 and can cause the deployablecushioning-device positioned on elongate structure 204 to deploy byexpanding with a gaseous substance.

In an example, system 200 can include sensors configured to measuretension of tether 208 during operation of UAV 206. Based on the measuredtension level of tether 208, the computing system of system 200 candetermine that UAV 206 is operating abnormally or preparing to execute alanding. In response, UAV 206 can cause deployable cushioning-device 228positioned on elongate structure 204 to deploy. Similarly, the computingsystem can also perform other operations based on the measured tensionlevel of tether 208. For example, the computing system of system 200 cancause a collapsible portion of landing structure 210 to extend outwardin order to prepare for the landing of UAV 206 or adjust a length oftether 208 using spooling mechanism 214.

In another example, the computing system of system 200 can receivesensor data from a sensor of UAV 206 that provides information regardingoperation of UAV 206. The computing system can make a determination thatthe received sensor data has a particular property, and detect abnormaloperation of UAV 206 based on the determination. Likewise, the computingsystem can determine other information regarding UAV 206 from sensordata received from sensors of UAV 206. For example, the computing systemcan receive an indication from UAV 206 that UAV 206 is decreasing inelevation and prepare for a landing by UAV 206. Likewise, computingsystem can receive sensor data indicating that UAV 206 is running low onbattery power. In the above situations and other possible scenarios, thecomputing system can cause one or multiple deployable cushioning-devicesto deploy as well as cause other components of system 200 to performoperations (e.g., prepare landing structure 210).

FIG. 4 is a flow chart illustrating an example method 400. At block 402,method 400 can include detecting abnormal operation of the UAV. At block404, method 400 can include responsive to detecting abnormal operationof the UAV, causing the deployable cushioning-device to deploy.

IV. Example Variations

Although some of the acts and/or functions described in this disclosurehave been described as being performed by a particular entity, such actsand/or functions can be performed by any entity, such as those describedin this disclosure. Further, although the described acts and/orfunctions have been recited in a particular order, the acts and/orfunctions need not be performed in the order recited. However, in someinstances, it can be desired to perform the acts and/or functions in theorder recited. Also, not all of the described acts and/or functions needto be performed to achieve one or more of the benefits provided by thisdisclosure, and therefore not all acts and/or functions are required.

Although certain variations have been discussed in connection with oneor more example of this disclosure, such variations can also be appliedto all of the other examples of this disclosure as well.

Although select examples of this disclosure have been described,alterations and permutations of these examples will be apparent to thoseof ordinary skill in the art. Other changes, substitutions, and/oralterations are also possible without departing from the invention inits broader aspects as set forth in the following claims.

1. A system comprising: a base comprising a bottom surface and a firstcoupling-point; a vertically-oriented elongate structure comprising alower end, an upper end, and an inner channel, wherein the inner channelcomprises an upper access-point disposed proximate the upper end,wherein the base is coupled to the elongate structure proximate thelower end; an unmanned aerial vehicle (UAV) comprising a secondcoupling-point; and a tether comprising a first portion, a secondportion, a third portion, and a fourth portion, wherein (i) the firstportion is coupled to the first coupling-point, (ii) the second portionis coupled to the second coupling-point, (iii) the third portion extendsthrough the inner channel, (iv) the fourth portion extends from theupper access-point to the second coupling-point, and (v) the fourthportion has a length that is less than a distance between the upperaccess-point and the bottom surface.
 2. The system of claim 1, whereinthe base comprises a vehicle.
 3. The system of claim 1, wherein the basecomprises a spooling mechanism configured for adjusting a length of thefourth portion, and wherein the first coupling-point is disposed on thespooling mechanism.
 4. The system of claim 1, wherein the base comprisesa power source, and wherein the tether is configured for deliveringpower from the power source to the UAV.
 5. The system of claim 1,wherein the base comprises a computing system, and wherein the tether isconfigured for facilitating communication between the computing systemand the UAV.
 6. The system of claim 1, wherein the vertically-orientedelongate structure comprises a mast having an adjustable height.
 7. Thesystem of claim 1, wherein the upper access-point is circular shaped. 8.A system for use with an unmanned aerial vehicle (UAV), the systemcomprising: a base comprising a first coupling-point; avertically-oriented elongate structure comprising a lower end, an upperend, and an inner channel, wherein the inner channel comprises an upperaccess-point disposed proximate the upper end, wherein the base iscoupled to the elongate structure proximate the lower end; a landingstructure constructed and arranged for receiving the UAV, wherein thelanding structure is coupled to the elongate structure proximate theupper end; and a tether comprising a first portion, a second portion, athird portion, and a fourth portion, wherein (i) the first portion iscoupled to the first coupling-point, (ii) the second portion is coupledto a second coupling-point of the UAV, (iii) the third portion extendsthrough the inner channel, and (iv) the fourth portion extends from theupper access-point and to the second coupling-point.
 9. The system ofclaim 8, wherein the base comprises a vehicle.
 10. The system of claim8, wherein the base comprises a spooling mechanism configured foradjusting a length of the fourth portion, and wherein the firstcoupling-point is disposed on the spooling mechanism.
 11. The system ofclaim 8, wherein the vertically-oriented elongate structure comprises amast having an adjustable height.
 12. The system of claim 8, wherein thelanding structure comprises a bowl-shaped portion.
 13. The system ofclaim 8, wherein the landing structure comprises a coupling portion thatextends around the upper end of the elongate structure to facilitatecoupling the landing structure to the elongate structure.
 14. The systemof claim 8, wherein the landing structure comprises an opening disposedproximate the upper access-point, and wherein at least one of the thirdportion and the fourth portion extends through the opening.
 15. Thesystem of claim 14, wherein the opening is disposed proximate a centerportion of the landing structure.
 16. The system of claim 14, whereinthe opening is circular shaped.
 17. The system of claim 8, wherein thelanding structure comprises a net disposed around a perimeter of thelanding structure.
 18. The system of claim 8, wherein at least a portionof the landing structure is collapsible.
 19. A system for use with anunmanned aerial vehicle (UAV), the system comprising: a base comprisinga bottom surface and a first coupling-point; a vertically-orientedelongate structure comprising a lower end, an upper end, and an innerchannel, wherein the inner channel comprises an upper access-pointdisposed proximate the upper end, wherein the base is coupled to theelongate structure proximate the lower end; a landing structureconstructed and arranged for receiving the UAV, wherein the landingstructure is coupled to the elongate structure proximate the upper end;and a tether comprising a first portion, a second portion, a thirdportion, and a fourth portion, wherein (i) the first portion is coupledto the first coupling-point, (ii) the second portion is coupled to asecond coupling-point of the UAV, (iii) the third portion extendsthrough the inner channel, (iv) the fourth portion extends from theupper access-point to the second coupling-point, and (v) the fourthportion has a length that is less than a distance between the upperaccess-point and the bottom surface.
 20. The system of claim 18, whereinthe landing structure comprises a bowl-shaped portion.